Ni-BASED SUPERALLOY WITH EXCELLENT OXIDIZATION RESISTANCE AND CREEP PROPERTY AND METHOD OF MANUFACTURING THE SAME

ABSTRACT

The present disclosure relates to a Ni-based superalloy with excellent oxidation resistance and creep properties, which is suitable for parts of energy plants and chemical plants under a corrosive oxidative/reductive atmosphere, which stainless steel cannot withstand, through adjustment of alloy components and control of process conditions and a method of manufacturing the same. The Ni-based superalloy includes: chromium (Cr): 20˜26 wt %, tungsten (W): 13˜17 wt %, molybdenum (Mo): 1˜5 wt %, manganese (Mn): 0.1˜1.0 wt %, silicon (Si): 0.1˜0.6 wt %, aluminum (Al): 0.1˜1.0 wt %, lanthanum (La): 0.01˜0.06 wt %, carbon (C): 0.01˜0.20 wt %, and the balance of nickel (Ni) and unavoidable impurities.

CROSS REFERENCE TO RELATED APPLICATION

This application claims the benefit of Korean patent application no. 10-2014-0164756, filed on Nov. 24, 2014, entitled “Ni-BASED SUPERALLOY WITH EXCELLENT OXIDIZATION RESISTANCE AND CREEP PROPERTY AND METHOD OF MANUFACTURING THE SAME”, which is hereby incorporated by reference in its entirety into this application.

BACKGROUND

1. Technical Field

The present invention relates to a Ni-based superalloy and a method of manufacturing the same, and more particularly, to a Ni-based superalloy with excellent oxidization resistance and creep properties, which is suitable for parts of energy plants and chemical plants under a corrosive oxidative/reductive atmosphere, which stainless steel cannot withstand, through adjustment of alloy components and control of process conditions, and a method of manufacturing the same.

2. Description of the Related Art

Superalloys refer to alloys which are mainly aimed at withstanding use at high temperature, and heat resistant steels refer to alloy steels which exhibit stable mechanical properties and good corrosion resistance even at high temperature.

Among wrought Ni-based superalloys, examples of commercially available alloys with good corrosion resistance and creep properties include Haynes 230 and Alloy 617, both of which can be used for long periods of time while exhibiting good phase stability up to about 650° C. In particular, in power generation equipment such as A-USC (Advanced-Ultra supercritical) equipment, the temperature of main steam can be increased from existing 650° C. to 700˜760° C. for reduction of carbon dioxide emission and energy efficiency. Since commercially available alloys are difficult to use at 700˜760° C., there is a need for novel alloys having good creep properties.

In addition, commercially available alloys have a problem in that the alloys cannot exhibit good creep properties and good oxidization resistance at the same time.

In the related art, Korean Patent Publication No. 10-1998-022301 (issued on Jul. 6, 1998) discloses Ni-based superalloys for casting.

BRIEF SUMMARY

It is an aspect of the present invention to provide a Ni-based superalloy with excellent oxidization resistance and creep properties, which is suitable for parts of energy plants and chemical plants under a corrosive oxidative/reductive atmosphere, which stainless steel cannot withstand, through adjustment of alloy components and control of process conditions, and a method of manufacturing the same.

In accordance with an aspect of the present invention, provided is a Ni-based superalloy with excellent oxidization resistance and creep properties, which includes chromium (Cr): 20˜26% by weight (wt %), tungsten (W): 13˜17 wt %, molybdenum (Mo): 1˜5 wt %, manganese (Mn): 0.1˜1.0 wt %, silicon (Si): 0.1˜0.6 wt %, aluminum (Al): 0.1˜1.0 wt %, lanthanum (La): 0.01˜0.06 wt %, carbon (C): 0.01˜0.20 wt %, and the balance of nickel (Ni) and unavoidable impurities.

In accordance with another aspect of the present invention, provided is a method of manufacturing a Ni-based superalloy with excellent oxidization resistance and creep properties, including: (a) preparing an alloy by mixing and dissolving raw materials including chromium (Cr): 20˜26 wt %, tungsten (W): 13˜17 wt %, molybdenum (Mo): 1˜5 wt %, manganese (Mn): 0.1˜1.0 wt %, silicon (Si): 0.1˜0.6 wt %, aluminum (Al): 0.1˜1.0 wt %, lanthanum (La): 0.01˜0.06 wt %, carbon (C): 0.01˜0.20 wt %, and the balance of nickel (Ni) and unavoidable impurities; (b) hot rolling the alloy; (c) annealing the hot rolled alloy; and (d) cooling the annealed alloy.

The Ni-based superalloy with excellent oxidization resistance and creep properties and the method of manufacturing the same according to the present invention can enhance creep properties by lowering the amounts of chromium (Cr) and silicon (Si), and improve oxidization resistance by excluding Fe while increasing the amount of manganese (Mn), thereby improving oxidization resistance and creep properties at the same time.

In addition, the Ni-based superalloy manufactured by the method according to the present invention exhibits excellent oxidization resistance and creep properties even at a high temperature of 700° C. or more through adjustment of alloy components and control of process conditions, and thus is suitable for parts of energy plants and chemical plants under a corrosive oxidative/reductive atmosphere, which stainless steel cannot withstand.

BRIEF DESCRIPTION OF THE DRAWINGS

The above and other aspects, features and advantages of the invention will become apparent from the detailed description in conjunction with the accompanying drawings, in which:

FIG. 1 is a flowchart of a method of manufacturing a Ni-based superalloy in accordance with one embodiment of the present invention;

FIG. 2 is a graph showing creep strain over time for samples prepared in Examples 1 to 6 and Comparative Example 2;

FIG. 3 is a graph showing creep results for samples prepared in Examples 1 to 6 and Comparative Examples 1 and 3; and

FIG. 4 is a graph showing cyclic oxidation property results for samples prepared in Example 1, Examples 7 to 11 and Comparative Example 2.

DETAILED DESCRIPTION

Embodiments of the present invention will now be described in detail with reference to the accompanying drawings. It should be understood that the present invention is not limited to the following embodiments and may be embodied in different ways, and that the embodiments are given to provide complete disclosure of the present invention and to provide thorough understanding of the present invention to those skilled in the art. The scope of the present invention is limited only by the accompanying claims and equivalents thereof. Like components will be denoted by like reference numerals throughout the specification.

Hereinafter, a Ni-based superalloy with excellent oxidization resistance and creep properties and a method of manufacturing the same according to embodiments of the invention will be described with reference to the accompanying drawings.

Ni-Based Superalloy

The Ni-based superalloy according to the present invention includes chromium (Cr): 20˜26 wt %, tungsten (W): 13˜17 wt %, molybdenum (Mo): 1˜5 wt %, manganese (Mn): 0.1˜1.0 wt %, silicon (Si): 0.1˜0.6 wt %, aluminum (Al): 0.1˜1.0 wt %, lanthanum (La): 0.01˜0.06 wt %, carbon (C): 0.01˜0.20 wt %, and the balance of nickel (Ni) and unavoidable impurities.

The Ni-based superalloy may further include 0.001˜0.015 wt % of boron (B).

Furthermore, the Ni-based superalloy has a yield strength (YS) of 195˜300 MPa, a tensile strength (TS) of 420˜580 MPa, and an elongation (El) of 35˜55% under temperature conditions of 700° C., and has a yield strength (YS) of 160˜200 MPa, a tensile strength (TS) of 235˜300 MPa, and an elongation (El) of 48˜59% under high temperature conditions of 900° C.

In development of the Ni-based superalloy with excellent oxidation resistance and creep properties according to the present invention, it was considered that decrease in chromium (Cr) content has an advantage in terms of improvement of creep properties, whereas increase in chromium (Cr) content has an advantage in terms of improvement of oxidation resistance. In this regard, the inventor has established an optimal composition range of chromium (Cr) which allows improvement in both oxidation resistance and creep properties at the same time. In addition, the inventor has found that appropriate amounts of tungsten (W) and molybdenum (Mo) can enhance creep properties, whereas an excess of tungsten (W) and molybdenum (Mo) causes deterioration in creep properties.

Thus, based on the established optimal composition ratio of alloy components, the present invention can enhance creep properties by lowering the amounts of chromium (Cr) and silicon (Si), and improve oxidation resistance by excluding Fe while increasing the amount of manganese (Mn), thereby improving oxidation resistance and creep properties at the same time.

As a result, the Ni-based superalloy with excellent oxidation resistance and creep properties according to embodiments of the present invention exhibits good oxidation resistance and creep properties even at high temperatures of 700° C. or more through adjustment of alloy components and control of process conditions, and thus is suitable for parts of energy plants and chemical plants under a corrosive oxidative/reductive atmosphere, which stainless steel cannot withstand.

Hereinafter, each component of the Ni-based superalloy according to the present invention will be described in detail in terms of functions and content thereof.

Chromium (Cr)

Chromium (Cr) serves to improve corrosion resistance and oxidation resistance. However, an excess of chromium can cause formation of carbides or topologically close packed (TCP) phases.

Thus, chromium (Cr) is preferably present in an amount of 20˜26 wt % based on the total weight of the Ni-based superalloy. If the content of chromium (Cr) is less than 20 wt %, there can be a problem in terms of corrosion resistance. If the content of chromium (Cr) exceeds 26 wt %, creep properties can be deteriorated, and a TCP phase, which has an adverse influence on mechanical properties, can be produced when exposed to high temperature for long time.

Tungsten (W)

Tungsten (W) is an element which improves high temperature strength and creep strength by solid-solution strengthening.

Tungsten (W) is preferably present in an amount of 13˜17 wt % based on the total weight of the Ni-based superalloy. If the content of tungsten (W) is less than 13 wt %, it is difficult to obtain the aforementioned effects of tungsten. If the content of tungsten (W) exceeds 17 wt %, there can be a problem of deterioration in toughness and flexibility as well as reduction in phase stability.

Molybdenum (Mo)

Molybdenum (Mo) is a solid-solution strengthening element and serves to improve high temperature tensile properties and creep properties. In addition, molybdenum (Mo) is bound to carbon to form M₆C type carbides at grain boundaries, thereby suppressing grain growth.

Molybdenum (Mo) is preferably present in an amount of 1˜5 wt % based on the total weight of the Ni-based superalloy. If the content of molybdenum (Mo) is less than 1 wt %, there can be a problem in that the solid-solution strengthening effect can hardly be obtained due to too low amount of molybdenum and creep properties can be deteriorated. If the content of molybdenum (Mo) exceeds 5 wt %, hot workability can be deteriorated and a TCP phase is likely to be formed.

Manganese (Mn)

Manganese (Mn) serves to improve oxidation resistance of alloys.

Manganese (Mn) is preferably present in an amount of 0.1˜1.0 wt % based on the total weight of the Ni-based superalloy. If the content of manganese (Mn) is less than 0.1 wt %, improvement in creep property can be insignificant due to too low amount of manganese. If the content of manganese (Mn) exceeds 1.0 wt %, there is a problem of deterioration in workability and oxidation resistance.

Silicon (Si)

Like manganese (Mn), silicon (Si) also improves oxidation resistance of alloys.

Silicon (Si) is preferably present in an amount of 0.1˜0.6 wt % based on the total weight of the Ni-based superalloy. If the content of silicon (Si) is less than 0.1 wt %, improvement in oxidation resistance can be insignificant due to too low amount of manganese. If the content of silicon (Si) exceeds 0.6 wt %, oxidation resistance can be improved, but creep properties can be sharply deteriorated.

Aluminum (Al)

Aluminum (Al) is an element forming austenite (γ′), which is a main reinforcing phase of the Ni-based superalloy, and contributes to improvement in oxidation resistance.

Aluminum (Al) is preferably present in an amount of 0.1˜10 wt % based on the total weight of the Ni-based superalloy. If the content of aluminum (Al) is less than 0.1 wt %, the aforementioned effects of aluminum are not obtained. If the content of aluminum (Al) exceeds 1.0 wt %, an excess of γ′ phase is precipitated, causing deterioration in workability.

Lanthanum (La)

Lanthanum (La) serves to improve oxidation resistance.

Lanthanum (La) is preferably present in an amount of 0.01˜0.06 wt % based on the total weight of the Ni-based superalloy. If the content of lanthanum (La) is less than 0.01 wt %, the aforementioned effects of lanthanum can hardly be obtained due to too low amount of lanthanum. If the content of lanthanum (La) exceeds 0.06 wt %, there can be a problem of deterioration in oxidation resistance due to interaction with boron (B).

Carbon (C)

Carbon (C) is bound with tungsten (W), molybdenum (Mo), chromium (Cr), and the like to form carbides in the form of MC, M₆C, or M₂₃C₆, and contributes to refinement of grains. In addition, carbon forms carbides at grain boundaries, thereby enhancing strength of the grain boundaries.

Carbon (C) is preferably present in an amount of 0.01˜0.20 wt % based on the total weight of the Ni-based superalloy. If the content of carbon (C) is less than 0.01 wt %, the strength enhancing effect can hardly be obtained due to insufficient formation of carbides. If the content of carbon (C) exceeds 0.20 wt %, an excess of carbides is formed, thereby causing deterioration in flexibility, workability, and the like.

Boron (B)

Boron (B) is segregated at grain boundaries to improve strength of the grain boundaries, and to suppress grain growth, thereby improving creep properties.

Boron (B) is preferably present in an amount of 0.001˜0.015 wt % based on the total weight of the Ni-based superalloy. If the content of boron (B) is less than 0.001 wt %, the creep property enhancing effect can hardly be obtained due to too low amount of boron. If the content of boron (B) exceeds 0.015 wt %, there is a problem of deterioration in oxidation resistance due to interaction with lanthanum (La) which serves to improve oxidation resistance.

Method of Manufacturing Ni-Based Superalloy

FIG. 1 is a flowchart of a method of manufacturing a Ni-based superalloy in accordance with one embodiment of the present invention.

Referring to FIG. 1, a process of manufacturing a Ni-based superalloy according to one embodiment of the invention includes preparing an alloy by mixing and dissolving raw materials (S110), hot rolling (S120), annealing (S130), and cooling (S140).

Mixing and Dissolving Raw Materials

In operation of preparing an alloy by mixing and dissolving raw materials (S110), the raw materials are mixed and dissolved, wherein the raw materials include chromium (Cr): 20˜26 wt %, tungsten (W): 13˜17 wt %, molybdenum (Mo): 1˜5 wt %, manganese (Mn): 0.1˜1.0 wt %, silicon (Si): 0.1˜0.6 wt %, aluminum (Al): 0.1˜1.0 wt %, lanthanum (La): 0.01˜0.06 wt %, carbon (C): 0.01˜0.20 wt %, and the balance of nickel (Ni) and unavoidable impurities. Here, an alloy in which these components are uniformly mixed may be prepared by mixing and dissolving the raw materials in a molten metal.

In this operation, the alloy may further include boron (B): 0.001˜0.015 wt %.

Hot Rolling

In operation of hot rolling (S120), the prepared alloy is subjected to hot rolling.

Here, hot rolling is preferably performed at a reduction rate of 40˜80% and at 1100˜1250° C. If the hot rolling temperature is less than 1100° C., there can be a problem in that the alloy is likely to suffer from cracking during hot rolling. Further, the hot rolling temperature exceeds 1250° C., there can be a problem in that it is difficult to control microstructure of the alloy due to grain coarsening of the alloy.

In addition, if the reduction rate in hot rolling is less than 40%, it is difficult to ensure a structure having both uniformity and fineness. If the reduction rate in hot rolling exceeds 80%, there is a problem in that hot rolling takes a long time, thereby causing low yield.

Annealing

In operation of annealing (S130), the hot rolled alloy is subjected to annealing.

Annealing may include solution annealing the hot rolled alloy at 1200˜1280° C., and aging the solution annealed alloy at 700° C.˜850° C. Aging is optionally performed depending upon the composition of the alloy.

Preferably, after solution annealing in which the hot rolled alloy is maintained in a high temperature range of 1100˜1280° C. for 5˜180 minutes, aging is carried out in a middle temperature range of 700˜850° C. for 4˜8 hours.

Here, when solution annealing is performed out of the range from 1100˜1280° C., precipitates are not sufficiently dissolved to provide desired properties. Preferably, solution annealing is performed for 5˜180 minutes, which allows carbide and γ′ precipitate phases within the alloy to be sufficiently dissolved in the alloy without causing grain growth.

In addition, aging is preferably performed at 700˜850° C. for 4˜8 hours such that the γ′ precipitate phases in the alloy are uniformly distributed in a matrix and the carbides are precipitated at grain boundaries to allow sufficient aging without change in a structure even when exposed to the same aging temperature range.

Cooling

In operation of cooling (S140), the annealed alloy is subjected to cooling.

Here, cooling may be performed to room temperature by water cooling or air cooling. Room temperature may range from 1° C. to 40° C., without being limited thereto.

Although not shown in FIG. 1, the method of manufacturing a Ni-based superalloy with good oxidation resistance and creep properties according to the embodiment may further include additional annealing (not shown) after cooling (S140).

In operation of additional annealing, the cooled alloy is subjected to additional annealing at 950˜1100° C. for 0.5˜4 hours. As a result, additional annealing after cooling (S140) can provide reinforced grain boundaries. Here, as additional annealing is performed, solid-solution strengthening alloy components such as carbon (C), chromium (Cr), and the like, produce precipitates to cause loss of solution strengthening effects. However, an additional precipitation strengthening effect resulting from additional annealing can counterbalance loss of the solution strengthening effects, thereby causing change in mechanical properties.

If the additional annealing temperature and time are out of the range as set forth above, stable precipitation cannot accomplished, which hinders production and growth of the precipitates. As a result, the desired effects cannot be sufficiently obtained.

The Ni-based superalloy manufactured through the above procedure can enhance creep properties by lowering the amounts of chromium (Cr) and silicon (Si), and improve oxidation resistance by excluding Fe while increasing the amount of manganese (Mn), thereby improving oxidation resistance and creep properties at the same time.

Moreover, the Ni-based superalloy manufactured by the method of the invention exhibits excellent oxidation resistance and creep properties even at a high temperature of 700° C. or more through adjustment of alloy components and control of process conditions, and thus is suitable for parts of energy plants and chemical plants under a corrosive oxidative/reductive atmosphere, which stainless steel cannot withstand.

Examples

Hereinafter, the present invention will be described with reference to some examples. However, these examples are given by way illustration only and should not be construed in any way as limiting the invention.

Descriptions of details apparent to those skilled in the art will be omitted herein.

1. Manufacture of Sample

Samples of Examples 1 to 11 and Comparative Examples 1 to 3 were prepared according to compositions as listed in Table 1 and process conditions as listed in Table 2.

TABLE 1 (unit: wt %) Cr W Mo Mn Si Al La C B Fe Co Ti Ni Example 1 21 14 2 0.7 0.2 0.2 0.02 0.1 0.015 — — — Bal. Example 2 26 16 2 0.8 0.3 0.5 0.02 0.1 0.015 — — — Bal. Example 3 23 14 4 0.1 0.5 0.2 0.02 0.1 0.015 — — — Bal. Example 4 21 14 2 0.7 0.2 0.2 0.04 0.04 0.005 — — — Bal. Example 5 26 16 2 0.8 0.3 0.5 0.02 0.16 0.005 — — — Bal. Example 6 23 14 4 0.1 0.5 0.2 0.04 0.04 0.005 — — — Bal. Example 7 21 14 2 0.7 0.2 0.5 0.02 0.1 0.015 — — — Bal. Example 8 21 14 2 0.7 0.2 0.8 0.02 0.1 0.015 — — — Bal. Example 9 21 14 2 0.7 0.5 0.2 0.02 0.1 0.015 — — — Bal. Example 10 21 14 2 0.7 0.5 0.5 0.02 0.1 0.015 — — — Bal. Example 11 21 14 2 0.7 0.5 0.8 0.02 0.1 0.015 — — — Bal. Comparative 22 14 2 0.5 0.4 0.3 0.02 0.1 0.015 3 5  — Bal. Example 1 Comparative 22 14 2 0.5 0.4 0.3 0.02 0.1 0.015 1.5 — — Bal. Example 2 Comparative 22 — 9 — — 1.2 — 0.07 — 1 12.5 0.3 Bal. Example 3

TABLE 2 Solution Hot rolling Reduction Solution annealing annealing temperature rate temperature time (° C.) (%) (° C.) (min) Example 1 1150 57 1135 60 Example 2 1150 58 1135 60 Example 3 1150 59 1135 60 Example 4 1150 61 1135 60 Example 5 1150 62 1135 60 Example 6 1150 59 1135 60 Example 7 1200 58 1135 60 Example 8 1200 61 1135 60 Example 9 1200 63 1135 60 Example 10 1200 64 1135 60 Example 11 1200 59 1135 60 Comparative 1150 56 1135 60 Example 1 Comparative 1150 62 1135 60 Example 2 Comparative 1150 55 1135 60 Example 3

2. Evaluation of Mechanical Properties

Table 3 shows evaluation results of mechanical properties of the samples prepared in Examples 1 to 11 and Comparative Examples 1 to 3.

TABLE 3 700° C. 900° C. YS TS EL YS TS EL (° C.) (° C.) (%) (° C.) (° C.) (° C.) Example 1 266 543 35.1 191 293 51.3 Example 2 302 583 38.1 160 240 59.8 Example 3 279 547 34.5 180 262 66.8 Example 4 193 423 55.4 161 235 54.6 Example 5 234 482 36.0 167 242 63.4 Example 6 234 490 39.8 176 259 48.4 Example 7 268 550 36.2 198 296 50.2 Example 8 271 561 35.2 201 302 50.6 Example 9 261 538 38.3 188 291 53.1 Example 10 270 544 34.1 195 301 54.1 Example 11 253 536 31.2 185 288 50.1 Comparative 252 593 62.1 199 280 96.5 Example 1 Comparative 240 531 59.2 185 252 89.9 Example 2 Comparative 241 553 78.9 175 253 96.5 Example 3

Referring to Tables 1 to 3, it can be seen that all of the samples of Examples 1 to 11 exhibited a yield strength (YS) of 195˜300 MPa, a tensile strength (TS) of 420˜580 MPa and an elongation (El) of 35˜55% under temperature conditions of 700° C., and satisfies a yield strength (YS) of 160˜200 MPa, a tensile strength (TS) of 235˜300 MPa and an elongation (El) of 48˜59% under high temperature conditions of 900° C.

On the other hand, it can be seen that the samples of Comparative Examples 1 to 3 exhibited yield strength (YS) and tensile strength (TS) as measured at 700° C. and 900° C., which were not much different than those of Examples 1 to 11. Thus, it can be seen that, despite not including cobalt (Co), the samples of Examples 1 to 11 exhibited similar mechanical properties in terms of high temperature strength to those of the samples of Comparative Examples 1 to 3.

FIG. 2 is a graph showing creep strain over time for samples prepared in Examples 1 to 6 and Comparative Example 2.

In FIG. 2, results of creep testing under conditions of 900° C. and 60 MPa show that the samples of Examples 2 to 6 had a shorter creep life than that of Comparative Example 2, which is a commercially available alloy. On the other hand, the samples of Example 1 had a final creep life of 1199 hours, which is about three times that of Comparative Example 2.

FIG. 3 is a graph showing creep property results for the samples of Examples 1 to 6 and Comparative Examples 1 and 3. In the graph showing stress according to LMP (Larson-Miller Parameter), a higher stress value at the same LMP indicates better creep properties.

In FIG. 3, it could be ascertained that the samples of Examples 2 to 6 did not exhibit better creep properties than those of Comparative Examples 1 and 3, whereas the sample of Example 1 exhibited better creep properties than those of Comparative Examples 1 and 3.

FIG. 4 is a graph showing cyclic oxidation property results for samples of Example 1, Examples 7 to 11 and Comparative Example 2, and more specifically, showing results obtained by a cyclic oxidation test in which the alloy samples of Example 1, Examples 7 to 11, and Comparative Example 2 were maintained at 1150° C. for 15 minutes, followed by maintaining the alloy samples at room temperature for 5 minutes.

In FIG. 4, it can be seen that all of samples in Example 1, Examples 7 to 11 and Comparative Example 2 tended to linearly decrease in weight over time. As a result, it can be seen that the samples of Example 1 and Examples 7 to 11 exhibited substantially similar oxidation resistance to the sample of Comparative Example 2, which is a commercially available alloy.

Although some embodiments have been described herein, it should be understood by those skilled in the art that these embodiments are given by way of illustration only, and that various modifications, variations, and alterations can be made without departing from the spirit and scope of the invention. Therefore, the scope of the invention should be limited only by the accompanying claims and equivalents thereof.

LIST OF REFERENCE NUMERALS

-   -   S110: Mixing and dissolving raw material     -   S120: Hot rolling     -   S130: Annealing     -   S140: Cooling 

What is claimed is:
 1. A Ni-based superalloy with excellent oxidation resistance and creep properties, comprising: chromium (Cr): 20˜26 wt %, tungsten (W): 13˜17 wt %, molybdenum (Mo): 1˜5 wt %, manganese (Mn): 0.1˜1.0 wt %, silicon (Si): 0.1˜0.6 wt %, aluminum (Al): 0.1˜1.0 wt %, lanthanum (La): 0.01˜0.06 wt %, carbon (C): 0.01˜0.20 wt %, and the balance of nickel (Ni) and unavoidable impurities.
 2. The Ni-based superalloy according to claim 1, further comprising: 0.001˜0.015 wt % of boron (B).
 3. The Ni-based superalloy according to claim 1, having a yield strength (YS) of 195˜300 MPa, a tensile strength (TS) of 420˜580 MPa, and an elongation (El) of 35˜55%, under temperature conditions of 700° C.
 4. The Ni-based superalloy according to claim 1, having a yield strength (YS) of 160˜200 MPa, a tensile strength (TS) of 235˜300 MPa, and an elongation (El) of 48˜59%, under high temperature conditions of 900° C.
 5. A method of manufacturing a Ni-based superalloy with excellent oxidation resistance and creep properties, comprising: (a) preparing an alloy by mixing and dissolving raw materials comprising chromium (Cr): 20˜26 wt %, tungsten (W): 13˜17 wt %, molybdenum (Mo): 1˜5 wt %, manganese (Mn): 0.1˜1.0 wt %, silicon (Si): 0.1˜0.6 wt %, aluminum (Al): 0.1˜1.0 wt %, lanthanum (La): 0.01˜0.06 wt %, carbon (C): 0.01˜0.20 wt %, and the balance of nickel (Ni) and unavoidable impurities; (b) hot rolling the alloy; (c) annealing the hot rolled alloy; and (d) cooling the annealed alloy.
 6. The method according to claim 5, wherein the alloy further comprises 0.001˜0.015 wt % of boron (B).
 7. The method according to claim 5, wherein hot rolling is performed at a reduction rate of 40˜80% and at 1100˜1250° C.
 8. The method according to claim 5, wherein annealing the hot rolled alloy comprises: (c-1) solution annealing the hot rolled alloy at 1200˜1280° C.; and (c-2) aging the solution annealed alloy at 700˜850° C.
 9. The method according to claim 5, further comprising: additionally annealing the cooled alloy at 950˜1100° C. for 0.5˜4 hours after cooling the annealed alloy. 